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Light and small UAV temperature and altitude test

Light and small UAV temperature and altitude test-Reliability Testing-

Test Background

Civilian light and small UAVs refer to UAV systems (including aircraft and ground stations) with a take-off weight between 0.25kg and 150kg. The temperature and altitude test of light and small UAVs can determine the ability of civilian light and small UAV systems to withstand the combined effects of temperature and altitude.
Zhongke Testing Reliability Experiment Center has environmental testing capabilities for various civilian light and small UAV systems, and provides professional temperature and altitude testing services for light and small UAVs.

Scope of tests

is suitable for civilian light and small UAV systems that may experience the combined environmental effects of temperature and altitude during use.

Test method

Determine the order of low temperature and low pressure test and high temperature and low pressure test according to relevant documents. Otherwise, perform low temperature and low pressure test first and then high temperature and low pressure test.

Test standard:

GB/T 38924.4-2020 Environmental test methods for civil light and small unmanned aerial vehicle systems Part 4: Temperature and altitude test
GB/T 2423.25-2008 Environmental testing of electrical and electronic products Part 2: Test method Test Z/AM: Low temperature/low pressure comprehensive test
GB/T 2423.26-2008 Environmental testing of electrical and electronic products Part 2: Test method Test Z/AM: High temperature/low pressure comprehensive test
GB/T 38924.1-2020 Environmental test methods for civil light and small unmanned aerial vehicle systems Part 1: General principles

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